IT1204308B - Ingresso per motore di aereo - Google Patents
Ingresso per motore di aereoInfo
- Publication number
- IT1204308B IT1204308B IT2013886A IT2013886A IT1204308B IT 1204308 B IT1204308 B IT 1204308B IT 2013886 A IT2013886 A IT 2013886A IT 2013886 A IT2013886 A IT 2013886A IT 1204308 B IT1204308 B IT 1204308B
- Authority
- IT
- Italy
- Prior art keywords
- entrance
- aircraft engine
- aircraft
- engine
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/0293—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turboprop engines
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
- Exhaust Gas After Treatment (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/791,830 US4607657A (en) | 1985-10-28 | 1985-10-28 | Aircraft engine inlet |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8620138A0 IT8620138A0 (it) | 1986-04-18 |
IT1204308B true IT1204308B (it) | 1989-03-01 |
Family
ID=25154920
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT2013886A IT1204308B (it) | 1985-10-28 | 1986-04-18 | Ingresso per motore di aereo |
Country Status (7)
Country | Link |
---|---|
US (1) | US4607657A (it) |
JP (1) | JPS61283729A (it) |
CA (1) | CA1250750A (it) |
DE (1) | DE3611803A1 (it) |
FR (1) | FR2589197B1 (it) |
GB (1) | GB2182100B (it) |
IT (1) | IT1204308B (it) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5203163A (en) * | 1990-08-01 | 1993-04-20 | General Electric Company | Heat exchange arrangement in a gas turbine engine fan duct for cooling hot bleed air |
GB2251031B (en) * | 1990-12-19 | 1995-01-18 | Rolls Royce Plc | Cooling air pick up |
GB9400555D0 (en) * | 1994-01-13 | 1994-03-09 | Short Brothers Plc | Boundery layer control in aerodynamic low drag structures |
DE10215551A1 (de) * | 2002-04-09 | 2003-10-23 | Rolls Royce Deutschland | Turboprop-Flugzeugtriebwerk |
WO2006091138A1 (en) * | 2005-02-25 | 2006-08-31 | Volvo Aero Corporation | A bleed structure for a bleed passage in a gas turbine engine |
JP4893110B2 (ja) * | 2006-05-31 | 2012-03-07 | 株式会社Ihi | 軸流流体装置 |
BRPI0906792A2 (pt) * | 2008-01-18 | 2015-07-14 | Ramgen Power Systems Llc | Método para iniciar um compressor de gás supersônico para comprimir um gás selecionado, e, compressor de gás supersônico |
GB201212072D0 (en) * | 2012-07-06 | 2012-08-22 | Rolls Royce Plc | Fluid intake and system for rotary machines |
CN112594087A (zh) * | 2012-10-23 | 2021-04-02 | 通用电气公司 | 无涵道的推力产生系统体系结构 |
US11300003B2 (en) | 2012-10-23 | 2022-04-12 | General Electric Company | Unducted thrust producing system |
GB201406952D0 (en) * | 2014-04-17 | 2014-06-04 | Rolls Royce Plc | Open rotor propulsion engine |
FR3032173B1 (fr) * | 2015-01-29 | 2018-07-27 | Safran Aircraft Engines | Pale d'helice de turbopropulseur a soufflage |
US11391298B2 (en) | 2015-10-07 | 2022-07-19 | General Electric Company | Engine having variable pitch outlet guide vanes |
US20180080476A1 (en) * | 2016-09-19 | 2018-03-22 | United Technologies Corporation | Geared turbofan front center body thermal management |
BE1024605B1 (fr) * | 2016-09-27 | 2018-04-26 | Safran Aero Boosters S.A. | Carter avec bras aspirant pour turbomachine axiale |
JP7333144B2 (ja) | 2018-03-16 | 2023-08-24 | ジョビー エアロ インク | 航空機抗力低減システム及び内部冷却電気モータ・システム並びにこれらを使用する航空機 |
US10808572B2 (en) * | 2018-04-02 | 2020-10-20 | General Electric Company | Cooling structure for a turbomachinery component |
US11492918B1 (en) * | 2021-09-03 | 2022-11-08 | General Electric Company | Gas turbine engine with third stream |
US11834995B2 (en) | 2022-03-29 | 2023-12-05 | General Electric Company | Air-to-air heat exchanger potential in gas turbine engines |
US11834954B2 (en) | 2022-04-11 | 2023-12-05 | General Electric Company | Gas turbine engine with third stream |
US11680530B1 (en) | 2022-04-27 | 2023-06-20 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with a power gearbox of a turbofan engine |
US11834992B2 (en) | 2022-04-27 | 2023-12-05 | General Electric Company | Heat exchanger capacity for one or more heat exchangers associated with an accessory gearbox of a turbofan engine |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR868609A (fr) * | 1939-10-13 | 1942-01-09 | B M W Flugmotorenbau G M B H | Dispositif pour influencer les conditions aérodynamiques sur le côté de courant d'impact de corps munis d'un revêtement, notamment de groupes propulseurs d'aéronefs |
FR932688A (fr) * | 1943-06-16 | 1948-03-30 | Vokes Ltd | Système d'épuration de l'air destiné aux moteurs et autres parties des avions |
DE864811C (de) * | 1944-12-14 | 1953-01-29 | Daimler Benz Ag | Verkleidung fuer Flugzeugtriebwerke mit vorn angeordneter Luftschraube |
GB645996A (en) * | 1948-10-21 | 1950-11-15 | Napier & Son Ltd | Improvements in or relating to air intakes for gas turbines and other internal combustion engines |
US2848155A (en) * | 1950-11-22 | 1958-08-19 | United Aircraft Corp | Boundary layer control apparatus for compressors |
US2931167A (en) * | 1953-02-06 | 1960-04-05 | Leduc Rene | Air intake arrangement for supersonic aircraft |
US3062484A (en) * | 1953-04-10 | 1962-11-06 | Curtiss Wright Corp | Supersonic air inlet construction |
BE535079A (it) * | 1954-01-25 | |||
US2841182A (en) * | 1955-12-29 | 1958-07-01 | Westinghouse Electric Corp | Boundary layer fluid control apparatus |
NL243195A (it) * | 1958-09-10 | 1900-01-01 | ||
GB1166733A (en) * | 1967-02-14 | 1969-10-08 | Minster Of Technology London | Aircraft Engine Intake Ducts |
GB1203963A (en) * | 1967-05-18 | 1970-09-03 | Mini Of Technology | Improvements relating to aircraft engine vortex suppressors |
GB1342590A (en) * | 1970-07-17 | 1974-01-03 | Secr Defence | Suppression of noise in gas turbine engines |
US3799475A (en) * | 1971-06-11 | 1974-03-26 | Nasa | Airflow control system for supersonic inlets |
US4007891A (en) * | 1975-09-12 | 1977-02-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Jet engine air intake system |
US4070827A (en) * | 1976-05-03 | 1978-01-31 | General Electric Company | Method and apparatus for limiting ingestion of debris into the inlet of a gas turbine engine |
-
1985
- 1985-10-28 US US06/791,830 patent/US4607657A/en not_active Expired - Fee Related
-
1986
- 1986-04-04 GB GB8608326A patent/GB2182100B/en not_active Expired - Fee Related
- 1986-04-08 DE DE19863611803 patent/DE3611803A1/de not_active Ceased
- 1986-04-10 FR FR8605105A patent/FR2589197B1/fr not_active Expired - Fee Related
- 1986-04-11 JP JP61082459A patent/JPS61283729A/ja active Granted
- 1986-04-18 IT IT2013886A patent/IT1204308B/it active
- 1986-09-18 CA CA000518558A patent/CA1250750A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
DE3611803A1 (de) | 1987-04-30 |
GB8608326D0 (en) | 1986-05-08 |
US4607657A (en) | 1986-08-26 |
JPH0580579B2 (it) | 1993-11-09 |
FR2589197A1 (fr) | 1987-04-30 |
GB2182100B (en) | 1990-04-11 |
CA1250750A (en) | 1989-03-07 |
IT8620138A0 (it) | 1986-04-18 |
JPS61283729A (ja) | 1986-12-13 |
GB2182100A (en) | 1987-05-07 |
FR2589197B1 (fr) | 1990-08-03 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
IT1204308B (it) | Ingresso per motore di aereo | |
IT1145460B (it) | Impianto elettrico di avviamento di motore di aereo di generazine | |
IT8421854V0 (it) | Veicolo senza motore per spostamenti di singole persone su brevi distanze. | |
IT1185624B (it) | Dispositivo di governo per aeromobili | |
DK317487A (da) | Overlappende klaebemiddelforbindelse | |
KR870006956U (ko) | 엔진의 냉각구조 | |
IT1173046B (it) | Supproto motore | |
DK514286D0 (da) | Spaendesystem | |
BR8605556A (pt) | Aviao conversivel | |
IT1211518B (it) | Motore particolarmente per velivoli ultraleggeri | |
FR2607915B1 (fr) | Systeme de guidage d'engin volant | |
IT8267130A0 (it) | Sopporto motore per aeromobili | |
IT1135845B (it) | Iniettore-pompa per motori diesel | |
AT384265B (de) | Getarnter hangar | |
IT1197092B (it) | Supporto per motore | |
KR860012796U (ko) | 물기 제거용 빗 | |
IT8548342A0 (it) | Aeromobile | |
IT8447671A0 (it) | Motore idro-gravitazionale | |
IT8647646A0 (it) | Motore idro-gravitazionale | |
BR6501469U (pt) | Motor multiplo | |
SE457329B (sv) | Flygfarkost | |
IT8735550V0 (it) | Aeroscivolante monomotore | |
BR8503370A (pt) | Motor helijato | |
SE8505279D0 (sv) | Flygande tefat | |
SE8503704D0 (sv) | Vertikal vindmotor |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19930415 |